View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 04603U 26088.19733545 +.00000000 +00000-0 +15605-2 0 00006
2 04603 99.4989 192.3855 0022181 108.1632 315.6095 13.87677897 03
| Epoch (UTC): | 29 March 2026 04:44:09 |
| Eccentricity: | 0.0022181 |
| inclination: | 99.4989° |
| perigee height: | 921 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 192.3855° |
| argument of perigee: | 108.1632° |
| revolutions per day: | 13.87677897 |
| mean anomaly at epoch: | 315.6095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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